20140601008979A

Accident · Substantial damage

FAA accident report · Cessna 182K · Galena, AK · June 1, 2014

Date
June 1, 2014 · 13:15 local
Place
Galena, AK
Airport
Galena
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2631R
NTSB investigation
NTSBANC14LA034
Reported as
Cessna 182K
Reported engine
Continental O-470 series
People aboard
4
Fatal injuries
0
Other injuries
4
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
750 total73 in this make and model25 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Ptrs #201402030

NTSB #anc 14 l a 034

While cruising at 1500' MSL the aircraft engine began to run rough, lose power, and subsequently quit. Prior to complete engine failure roughness was described as the engine reving up and down, sputtering, and cutting in and out.

Emergency landing was made along a lake shore.

Aircraft flipped over on landing and was partially submerged.

Minor injuries initially reported, including the pilot and one passenger. The one passenger did seek medical attention at fairbanks memorial hospital within 24 hours of the accident. The other two passengers claimed injuries at a later date.

Fuel exhaustion suspected as both fuel gauges described as reading empty by pilot and passengers with little or no fluctuation of fuel gauge needles when the engine quit.

This was in conflict with electronic totalizer indicating 22.8 gallons remaining. Fuel totalizer was set incorrectly with 82 gallons usable, aircraft only holds 79 gallons useable. This discrepancy however would not have resulted in fuel exhaustion.

Upon examination of fuel tanks it was discovered that at least eight fuel tank bladder rettention buttons (5 in left wing, 3 on the right) were not connected. This condition could have been caused by the accident, or post crash movement. If, however these retention buttons were not in place when the aircraft was fueled for this flight a false full fuel indication may have resulted.

On 01/16/2014 chena marina air service discovered 6 fuel bladder fuel snaps on one side and one on antoher had come unsnapped. They repaired the snaps prior to returning to the owner, who after these repairs, leased the aircraft to the yukon river tribal council. The aircraft was flown 72.3 hours between the repair time and time of the accident.

An estimated 8.8 to 11.7 gallons of fuel should have remained in the tanks which would have met the requirements to complete the planned flight. Unsecured bladder retention buttons could account for this fuel shortage.

As the FAA filed it

PTRS #201402030

NTSB #ANC 14 L A 034

WHILE CRUISING AT 1500' MSL THE AIRCRAFT ENGINE BEGAN TO RUN ROUGH, LOSE POWER, AND SUBSEQUENTLY QUIT. PRIOR TO COMPLETE ENGINE FAILURE ROUGHNESS WAS DESCRIBED AS THE ENGINE REVING UP AND DOWN, SPUTTERING, AND CUTTING IN AND OUT.

EMERGENCY LANDING WAS MADE ALONG A LAKE SHORE.

AIRCRAFT FLIPPED OVER ON LANDING AND WAS PARTIALLY SUBMERGED.

MINOR INJURIES INITIALLY REPORTED, INCLUDING THE PILOT AND ONE PASSENGER. THE ONE PASSENGER DID SEEK MEDICAL ATTENTION AT FAIRBANKS MEMORIAL HOSPITAL WITHIN 24 HOURS OF THE ACCIDENT. THE OTHER TWO PASSENGERS CLAIMED INJURIES AT A LATER DATE.

FUEL EXHAUSTION SUSPECTED AS BOTH FUEL GAUGES DESCRIBED AS READING EMPTY BY PILOT AND PASSENGERS WITH LITTLE OR NO FLUCTUATION OF FUEL GAUGE NEEDLES WHEN THE ENGINE QUIT.

THIS WAS IN CONFLICT WITH ELECTRONIC TOTALIZER INDICATING 22.8 GALLONS REMAINING. FUEL TOTALIZER WAS SET INCORRECTLY WITH 82 GALLONS USABLE, AIRCRAFT ONLY HOLDS 79 GALLONS USEABLE. THIS DISCREPANCY HOWEVER WOULD NOT HAVE RESULTED IN FUEL EXHAUSTION.

UPON EXAMINATION OF FUEL TANKS IT WAS DISCOVERED THAT AT LEAST EIGHT FUEL TANK BLADDER RETTENTION BUTTONS (5 IN LEFT WING, 3 ON THE RIGHT) WERE NOT CONNECTED. THIS CONDITION COULD HAVE BEEN CAUSED BY THE ACCIDENT, OR POST CRASH MOVEMENT. IF, HOWEVER THESE RETENTION BUTTONS WERE NOT IN PLACE WHEN THE AIRCRAFT WAS FUELED FOR THIS FLIGHT A FALSE FULL FUEL INDICATION MAY HAVE RESULTED.

ON 01/16/2014 CHENA MARINA AIR SERVICE DISCOVERED 6 FUEL BLADDER FUEL SNAPS ON ONE SIDE AND ONE ON ANTOHER HAD COME UNSNAPPED. THEY REPAIRED THE SNAPS PRIOR TO RETURNING TO THE OWNER, WHO AFTER THESE REPAIRS, LEASED THE AIRCRAFT TO THE YUKON RIVER TRIBAL COUNCIL. THE AIRCRAFT WAS FLOWN 72.3 HOURS BETWEEN THE REPAIR TIME AND TIME OF THE ACCIDENT.

AN ESTIMATED 8.8 TO 11.7 GALLONS OF FUEL SHOULD HAVE REMAINED IN THE TANKS WHICH WOULD HAVE MET THE REQUIREMENTS TO COMPLETE THE PLANNED FLIGHT. UNSECURED BLADDER RETENTION BUTTONS COULD ACCOUNT FOR THIS FUEL SHORTAGE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.